US3509614A - Method of making a filament wheel - Google Patents
Method of making a filament wheel Download PDFInfo
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- US3509614A US3509614A US658784A US3509614DA US3509614A US 3509614 A US3509614 A US 3509614A US 658784 A US658784 A US 658784A US 3509614D A US3509614D A US 3509614DA US 3509614 A US3509614 A US 3509614A
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- wheel
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- filament
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
- B29C37/0003—Discharging moulded articles from the mould
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/56—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits
- B29C65/562—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using mechanical means or mechanical connections, e.g. form-fits using extra joining elements, i.e. which are not integral with the parts to be joined
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/128—Stepped joint cross-sections
- B29C66/1282—Stepped joint cross-sections comprising at least one overlap joint-segment
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/12—Joint cross-sections combining only two joint-segments; Tongue and groove joints; Tenon and mortise joints; Stepped joint cross-sections
- B29C66/128—Stepped joint cross-sections
- B29C66/1284—Stepped joint cross-sections comprising at least one butt joint-segment
- B29C66/12841—Stepped joint cross-sections comprising at least one butt joint-segment comprising at least two butt joint-segments
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/50—General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
- B29C66/51—Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
- B29C66/54—Joining several hollow-preforms, e.g. half-shells, to form hollow articles, e.g. for making balls, containers; Joining several hollow-preforms, e.g. half-cylinders, to form tubular articles
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/72—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined
- B29C66/723—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the structure of the material of the parts to be joined being multi-layered
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
- B29C70/34—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/347—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation combined with compressing after the winding of lay-ups having a non-circular cross-section, e.g. flat spiral windings
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/40—Shaping or impregnating by compression not applied
- B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
- B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/28—Shaping operations therefor
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
- B29C70/545—Perforating, cutting or machining during or after moulding
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/0032—Producing rolling bodies, e.g. rollers, wheels, pulleys or pinions
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60B—VEHICLE WHEELS; CASTORS; AXLES FOR WHEELS OR CASTORS; INCREASING WHEEL ADHESION
- B60B5/00—Wheels, spokes, disc bodies, rims, hubs, wholly or predominantly made of non-metallic material
- B60B5/02—Wheels, spokes, disc bodies, rims, hubs, wholly or predominantly made of non-metallic material made of synthetic material
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
- B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2031/00—Other particular articles
- B29L2031/32—Wheels, pinions, pulleys, castors or rollers, Rims
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49481—Wheel making
- Y10T29/49492—Land wheel
- Y10T29/49496—Disc type wheel
- Y10T29/49503—Integral rim and disc making
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49789—Obtaining plural product pieces from unitary workpiece
- Y10T29/49794—Dividing on common outline
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49789—Obtaining plural product pieces from unitary workpiece
- Y10T29/49796—Coacting pieces
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49826—Assembling or joining
- Y10T29/49893—Peripheral joining of opposed mirror image parts to form a hollow body
Definitions
- FIGURE 1 there is shown a wheel construction that is made up from a first resin encased filament section 12 and a second resin encased filament section 14, each of which is provided with an upper surface 16 or 18 and a lower surface 20 or 22 that are respectively joined by center body portions 24 and 26.
- the center body portions 24 and 26 are joined together by a plurality of equidistantly arranged bolts 28 that pull the sections together upon the tightening of nuts 30 therefor.
- annular reinforcing rings 32 and 34 Underneath the bolt heads and the nuts there is provided annular reinforcing rings 32 and 34, to prevent the bolt heads and/or nuts from digging into the resin encased filament sections 12 or 14, and to provide more uniform stress distribution. Rings 32 and 34 may be loose or bonded to portions 24 and 26.
- annular sealing ring 36 to seal the assembly of the sec-' tions 12 and 14.
- annular sealing ring 36 may also be provided in this ring 36 a means for communicating fluid pressure from externally of the wheel through the ring 36 to the chamber of the tire that mav be mounted thereon (not shown) such 4 Claims as by means of a valve stem 38 that performs the dual function of a tightening means for joining the sections 12 and 14 and due to the internal passage 40 thereof that communicates with-an outwardly directed passage 42 in the ring 36 provides the fluid communication aforementioned.
- the ring 36 is provided with a plurality of grooves on opposite faces thereof into which appropriate seals 44 and 46, such as O-rings may be inserted to complete the sealing of the juncture of the sections 12 and 14.
- FIGURE 2 there is shown a similar wheel construction having first and second sections 60 and 62, respectively, joined by the bolt 61 for a nut 66 with Patented May 5, 1970 bearing or washer rings 68 and 70, as in FIGURE 1.
- the wheel is provided with right and left bearings 72 and 74 which are placed against the depending stops 76 and 78 of the lowermost surfaces of the wheel sections. These bearings support the wheel from an axle 80, and appropriate dust covers 82 and 84 are bolted to the wheel sections to prevent contamination of the bearings.
- FIGURE 2 the first and second sections 60 and 62 are shown in slightly enlarged detail so that the filaments 86 may be seen in the cross sectional cut to be surrounded by resin 88.
- the filaments 86 and resin 88 are generally wrapped to cover a surface of a toroid with a helical pattern of filaments with layers of resin running in one direction first and then in another to form multiple encased filaments.
- the wrapping of the filaments may be at a constant angle or at different angles dependent on the shape and loading required for the wheel.
- a pair of annular beads 90 and 92 are bonded by a high shear strength bond composition 94 to the uppermost surfaces of the sections 60 and 62. It
- the beads 90 and/ or 92 be formed to have a flat inner surface 96 and 98 that will mate with the upper or outer surfaces of the sections 60 and 62.
- the upper or outer surfaces 100 or 102 are formed to have a slight upward angle which, for example, has thus far been programmed as a 5 degree taper from the inner to the outermost portions of the upper surface to give a general convexprofile to the wheel.
- the flat inner surfaces 96 and 98 of the beads 90 and 92 are dimensioned to have a lesser internal diameter than the external diameter of the edges of the section 60, 62 so that the fiat surfaces 96 and 98 will create inward forces on the outermost edges of the section 60-and '62 upon the bonding thereto.
- the method of construction for manufacturing a wheel in accordance with the foregoing description is to first wind a tape or band of resin encased filaments in a toroidal shape upon a suitable mandrel as seen in FIGURE 5,"
- rings 108 and 110 may have beenpreviously fabricated by a spiral wrap about a foam or other type permanent core and cured or partially cured.
- the cross section of rings 108 and 110 may be round, of a D-shape or any other variation including the open C-section of FIGURE 1. If they are preformed, then they are slipped over the primary toroidal fabrication of filaments and resin and wedged up against the tapered center portion with a gap left between them (as illustrated in FIGURE 3).
- auxiliary rings may be then further aflixed by additional circumferential windings, if desired, or merely bonded in place with a resin.
- the entire assembly is then cured in an oven for a suitable time at a predetermined temperature to etfect proper curing of the thermo-setting type resin used. While curing, the assembly (in a preferred method of fabrication) is placed in a curing mold having sections 107 and 109 joined annularly by bolts 111 that will encapsulate the toroid and be adjustable during the curing process by the tightening of bolts 111 so as to size the wrapped product to assure that the external radial faces will be flat and true having a predetermined theoretically desired density.
- spaces 113 are provided centrally to permit escape of excess resins, and the molds will further position rings 108 and 110.
- the bolts 111 are removed and air is introduced via fittings 115 to cause pistons 116 to release the sections 107 and 109 from the wrapped product so that it may then be cut in two halves along the vertical centerline 112 on the inside and outside peripheries, as at 114 and 116. Further machining may be done at this time or later to make the inside faces of suitable shape for bearing seats, such as the formation of the depending stops 76 and 78 (see FIGURE 2) for anti-friction or other type bearings.
- This cutting and reversing of the toroid is one of the primary features which leads to an economical practice of the invention in that it provides a high strength filament wound structure of the proper shape and properties particularly suitable for mounting pneumatic tires, bearings and carrying the associated loads.
- this I may be secured by utilizing a filament of high tensile modulus of elasticity or by laying suitable core material between the inner and outer layers of the reinforcing filaments during winding.
- reinforcing inserts 124 (see FIGURE 2) by attaching it to the assembled wheel to provide an additional support for the stops 76 and 78.
- This tube could be made from metal stock or preferably fabricated from reinforced plastic to provide the desired strength-to-weight ratio.
- a bearing insert 126 may be fitted and joined, when desired, to the area of the wheel overlying the bearings for additional support.
- a method of forming a wheel comprising the steps of:
- a method of forming a wheel according to claim 3 wherein the wrapping of multiple layers of resin encased filaments includes the step of laying said filaments on said toroidal mandrel in a spiral pattern so that the filaments are provided with optimum load carrying ability.
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- Engineering & Computer Science (AREA)
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- Moulding By Coating Moulds (AREA)
Description
May 5, 1970 W. E. ELDRED METHOD OF MAKING A FILAMENT WHEEL Original Filed Jan. 17. 1966 3 Sheets-Sheet 1 INVENTOR.
WENDELL E. ELDRED BY W M'M ATTORNEYJ y 5, 1970 w. E. ELDRED 3,509,614
METHOD OF MAKING A FILAMENT WHEEL Original Filed Jan. 17. 1966 3 Sheets-Sheet 2 INVENTOR. WE/VDELL E. ELDAED A T TORNE Y3 May 5, 1970 w. E. ELDRED METHOD OF MAKING A FILAMENT WHEEL Original Filed Jan. 17. 1966 3 Sheets-Sheet 5 INVENTOR.
WENDELL E. ELDRED ATTORNEYS United States, Patent F 3,509,614 METHOD OF MAKING A FILAMENT WHEEL Wendell E. Eldred, South Bend, Ind., assignor to The Bendix Corporation, a corporation of Delaware Original application Jan. 17, 1966, Ser. No. 521,089, now Patent No. 3,357,747, dated Dec. 12, 1967. Divided and this application Aug. 7, 1967, Ser. No. 658,784
Int. Cl. B21d 53/26; B21k 1/28 U.S. Cl. 29-159 ABSTRACT OF THE DISCLOSURE A method for constructing a filament wheel comprising bands of filaments integrated by a binder wrapped into a toroidal body thereafter severed providing sections that are placed back-to-back with their severed edges facing outwardly and joined.
RELATED PATENTS This application is a divisional application of US. patent application Ser. No. 521,089 filed Jan. 17, 1966, now Patent No. 3,357,747.
SUMMARY In the fabrication of high strength structures from reinforced plastics, there are a variety of fabrication techniques with a large range of physical properties. Of the many methods, filament winding has proved to be far the strongest. Therefore, it is a principal object of this invention to provide a wheel construction which utilizes resin encased filaments to provide a lightweight, strong and yet economical wheel.
DRAWING DESCRIPTION mold during the fabrication of a wheel in accordance with I the principles of my invention.
DETAILED DESCRIPTION With more particular regard to FIGURE 1, there is shown a wheel construction that is made up from a first resin encased filament section 12 and a second resin encased filament section 14, each of which is provided with an upper surface 16 or 18 and a lower surface 20 or 22 that are respectively joined by center body portions 24 and 26.
The center body portions 24 and 26 are joined together by a plurality of equidistantly arranged bolts 28 that pull the sections together upon the tightening of nuts 30 therefor. Underneath the bolt heads and the nuts there is provided annular reinforcing rings 32 and 34, to prevent the bolt heads and/or nuts from digging into the resin encased filament sections 12 or 14, and to provide more uniform stress distribution. Rings 32 and 34 may be loose or bonded to portions 24 and 26.
Between the center bodies there may be provided an annular sealing ring 36 to seal the assembly of the sec-' tions 12 and 14. There may also be provided in this ring 36 a means for communicating fluid pressure from externally of the wheel through the ring 36 to the chamber of the tire that mav be mounted thereon (not shown) such 4 Claims as by means of a valve stem 38 that performs the dual function of a tightening means for joining the sections 12 and 14 and due to the internal passage 40 thereof that communicates with-an outwardly directed passage 42 in the ring 36 provides the fluid communication aforementioned.
Furthermore, the ring 36 is provided with a plurality of grooves on opposite faces thereof into which appropriate seals 44 and 46, such as O-rings may be inserted to complete the sealing of the juncture of the sections 12 and 14.
To the upper surfaces 16 and 18, there is bonded thereto a pair of rings 48 and 50, as at 52 and 54, by a high shear bonding substance. On the inner surfaces 20 and 22 of the respective sections 12 and 14, there is also provided depending stops 56 and 58 for the insertion of bearings to support the wheel 10 on an axle.
With regard to FIGURE 2, there is shown a similar wheel construction having first and second sections 60 and 62, respectively, joined by the bolt 61 for a nut 66 with Patented May 5, 1970 bearing or washer rings 68 and 70, as in FIGURE 1.
Furthermore, the wheel is provided with right and left bearings 72 and 74 which are placed against the depending stops 76 and 78 of the lowermost surfaces of the wheel sections. These bearings support the wheel from an axle 80, and appropriate dust covers 82 and 84 are bolted to the wheel sections to prevent contamination of the bearings.
In FIGURE 2 the first and second sections 60 and 62 are shown in slightly enlarged detail so that the filaments 86 may be seen in the cross sectional cut to be surrounded by resin 88. The filaments 86 and resin 88 are generally wrapped to cover a surface of a toroid with a helical pattern of filaments with layers of resin running in one direction first and then in another to form multiple encased filaments. The wrapping of the filaments may be at a constant angle or at different angles dependent on the shape and loading required for the wheel.
As in FIGURE 1, a pair of annular beads 90 and 92 are bonded by a high shear strength bond composition 94 to the uppermost surfaces of the sections 60 and 62. It
. is preferred, although not necessarily required, that the beads 90 and/ or 92 be formed to have a flat inner surface 96 and 98 that will mate with the upper or outer surfaces of the sections 60 and 62. Furthermore, the upper or outer surfaces 100 or 102 are formed to have a slight upward angle which, for example, has thus far been programmed as a 5 degree taper from the inner to the outermost portions of the upper surface to give a general convexprofile to the wheel. At the same time, the flat inner surfaces 96 and 98 of the beads 90 and 92 are dimensioned to have a lesser internal diameter than the external diameter of the edges of the section 60, 62 so that the fiat surfaces 96 and 98 will create inward forces on the outermost edges of the section 60-and '62 upon the bonding thereto.
This will have the effect of providing a wedge fit'between-i the beads 90 and 92 and the sections 60 and 62, respectively, that will be further enhanced when a tire is mounted and inflated on'the wheel.
The method of construction for manufacturing a wheel in accordance with the foregoing description is to first wind a tape or band of resin encased filaments in a toroidal shape upon a suitable mandrel as seen in FIGURE 5,"
having two sections 104 and 106.It should be notedthat the outermost surfaces of the shells 1'04 and 106-are pro--- vided-with an incline to allow the finished laminate of filaments 86 and resin 88 to have-an outer surface which-,-
isaugled upwardly toward the center of the toroidal mandrel. After the winding of the band of filaments 86 and the encasing resin 88, about the shells 104 and 106 by manner as to the beads aforedescribed, and which rings 108 and 110 may have beenpreviously fabricated by a spiral wrap about a foam or other type permanent core and cured or partially cured. The cross section of rings 108 and 110 may be round, of a D-shape or any other variation including the open C-section of FIGURE 1. If they are preformed, then they are slipped over the primary toroidal fabrication of filaments and resin and wedged up against the tapered center portion with a gap left between them (as illustrated in FIGURE 3). These auxiliary rings may be then further aflixed by additional circumferential windings, if desired, or merely bonded in place with a resin. The entire assembly is then cured in an oven for a suitable time at a predetermined temperature to etfect proper curing of the thermo-setting type resin used. While curing, the assembly (in a preferred method of fabrication) is placed in a curing mold having sections 107 and 109 joined annularly by bolts 111 that will encapsulate the toroid and be adjustable during the curing process by the tightening of bolts 111 so as to size the wrapped product to assure that the external radial faces will be flat and true having a predetermined theoretically desired density. In this regard, spaces 113 are provided centrally to permit escape of excess resins, and the molds will further position rings 108 and 110. Upon completion of the curing and cooling, the bolts 111 are removed and air is introduced via fittings 115 to cause pistons 116 to release the sections 107 and 109 from the wrapped product so that it may then be cut in two halves along the vertical centerline 112 on the inside and outside peripheries, as at 114 and 116. Further machining may be done at this time or later to make the inside faces of suitable shape for bearing seats, such as the formation of the depending stops 76 and 78 (see FIGURE 2) for anti-friction or other type bearings. These two halves are then reversed and placed back-to-back with their open sides out so that the original outside faces that are closed are abutting each other and are clamped together by a suitable number of bolts, as aforedescribed; and a pair of circumferential rings, which may be of metal or other suitable materials including reinforced plastic, can be used as shown.
This cutting and reversing of the toroid is one of the primary features which leads to an economical practice of the invention in that it provides a high strength filament wound structure of the proper shape and properties particularly suitable for mounting pneumatic tires, bearings and carrying the associated loads.
While the invention was primarily conceived for aircraft wheels, it would also prove quite suitable for many other types of wheels utilizing both solid and pneumatic tires wherever lightweight and high strength is required. Some of the advantages of the invention are as follows:
(1) A very high strength-to-Weight ratio that can be varied to meet the needs of the industry in accordance with predetermined specifications.
(2) Adaptable for both symmetrical and unsymmetrical wheels.
(3) Ability to supply ample space for brakes within the wheel contour.
(4) Suitable for low cost production by high speed automated winding machines.
(5) Provide wheels with thermal conductivity much lower than present wheel that will protect the tires from brake heat.
(6) Easily adapted to utilization of supporting axial reinforcing cross tubes.
(7) Readily attached reinforcements for brake key ways or other parts as required.
(8) Eliminates problems of corrosion encountered frequently in aircraft service.
(9) Can be designed for varying degrees of flexibility so that obstacles such as cables on carrier base ships can be swallowed without permanent set.
(10) Conversely, if additional stiffness is required, this I may be secured by utilizing a filament of high tensile modulus of elasticity or by laying suitable core material between the inner and outer layers of the reinforcing filaments during winding.
(11) Expensive and long lead time forging dies are eliminated.
In accordance with the advantage of paragraph (5) above and while the construction previously described is one which will be of lesser heat conductivity than any of the previous wheels known in the prior art, it may be required to further provide heat protection for a wheel and in so doing, it is quite feasible to interpose, in the various layers, reflective foils or heat barrier material as well as to coat or bond a heat reflective substance to the underneath side of the tapered upper surfaces for the wheel sections. As seen in FIGURE 2, such a practice could well entail the insertion of a reinforcement 122 during the wrapping process which will enable altering the strength-to-weight ratio while providing secondarily a heat barrier within the wheel.
In some wheel designs it may :be necessary to utilize reinforcing inserts 124 (see FIGURE 2) by attaching it to the assembled wheel to provide an additional support for the stops 76 and 78. This tube could be made from metal stock or preferably fabricated from reinforced plastic to provide the desired strength-to-weight ratio. In addition, a bearing insert 126 may be fitted and joined, when desired, to the area of the wheel overlying the bearings for additional support.
As I have mentioned previously, this invention is not intended to be limited to the particular feature aforedescribed, but is rather to have its meets and bounds set by the following claims.
I claim:
1. A method of forming a wheel comprising the steps of:
wrapping multiple layers of resin encased filaments about a toroidal mandrel;
dividing said layers of filaments into two sections each of which has an open end and a closed end;
placing said sections with their closed ends in abutting relationship; and
joining said abutting closed ends together.
2. A method of forming a wheel according to claim 1 and further comprising the step of placing annular rings on the outermost layer of the multiple layers of filaments in towards the center of the toroidal mandrel.
3. A method of forming a reinforced plastic wheel according to claim 2 and further comprising the step of placing said multiple layers of filaments and said rings in a compression mold to size said multiple layers and locate said rings with means to remove excess resin and cure said resin encased filaments prior to the step of dividing said layers into two sections.
4. A method of forming a wheel according to claim 3 wherein the wrapping of multiple layers of resin encased filaments includes the step of laying said filaments on said toroidal mandrel in a spiral pattern so that the filaments are provided with optimum load carrying ability.
References Cited UNITED STATES PATENTS 968,272 8/1910 Sextone 29-416 2,120,881 6/1938 Assbroicher et al 29-416 2,448,114 8/ 1948 Olson et al. 156-189 2,998,282 8/ 1961 Moyer.
3,023,135 2/1962 Wiltshire 156-189 XR 3,369,843 2/1968 Prew 301-63 3,423,816 1/1969 Crosh et al. 29-416 CHARLIE T. MOON, Primary Examiner US. Cl. X.R. 29-415, 416, 463
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US521089A US3357747A (en) | 1966-01-17 | 1966-01-17 | Filament wheel |
US65878467A | 1967-08-07 | 1967-08-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
US3509614A true US3509614A (en) | 1970-05-05 |
Family
ID=27060367
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US658784A Expired - Lifetime US3509614A (en) | 1966-01-17 | 1967-08-07 | Method of making a filament wheel |
Country Status (1)
Country | Link |
---|---|
US (1) | US3509614A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS51107902A (en) * | 1975-03-14 | 1976-09-24 | Takamasa Yamaura | SUIDENYOTORAKUTAANOSHARINNOKAIRYO |
US4213234A (en) * | 1976-04-20 | 1980-07-22 | Dunlop Limited | Method and apparatus for manufacturing vehicle wheel rims from spirally wound sheet metal |
EP0065086A1 (en) * | 1981-05-15 | 1982-11-24 | Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung | Rotating member |
DE3119500A1 (en) * | 1981-05-15 | 1983-01-27 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Rotatable body |
EP0083244A1 (en) * | 1981-12-28 | 1983-07-06 | Ford Motor Company Limited | Fibre reinforced synthetic material wheel |
FR2565159A1 (en) * | 1984-05-30 | 1985-12-06 | Aerospatiale | METHOD FOR MANUFACTURING A COMPONENT PIECE OF FILAMENTARY WINDING STRUCTURE AND PART THEREOF |
US4691431A (en) * | 1984-10-31 | 1987-09-08 | Sumitomo Rubber Industries, Ltd. | Method of making a metal mold for tire vulcanization |
EP2143635A2 (en) | 2008-07-07 | 2010-01-13 | Honeywell International Inc. | Hybrid aircraft wheel having metal and composite portions |
CN111923452A (en) * | 2020-06-22 | 2020-11-13 | 成都飞机工业(集团)有限责任公司 | Forming method for controlling curing deformation of composite material hyperboloid skin |
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US2120881A (en) * | 1935-11-28 | 1938-06-14 | Continental Gummi Werke Ag | Method of making molds |
US2448114A (en) * | 1943-05-18 | 1948-08-31 | Goodrich Co B F | Method for making heat-molded articles containing fabric reinforcements |
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Publication number | Priority date | Publication date | Assignee | Title |
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JPS51107902A (en) * | 1975-03-14 | 1976-09-24 | Takamasa Yamaura | SUIDENYOTORAKUTAANOSHARINNOKAIRYO |
US4213234A (en) * | 1976-04-20 | 1980-07-22 | Dunlop Limited | Method and apparatus for manufacturing vehicle wheel rims from spirally wound sheet metal |
EP0065086A1 (en) * | 1981-05-15 | 1982-11-24 | Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung | Rotating member |
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EP2143635A2 (en) | 2008-07-07 | 2010-01-13 | Honeywell International Inc. | Hybrid aircraft wheel having metal and composite portions |
EP2143635A3 (en) * | 2008-07-07 | 2012-03-28 | Honeywell International Inc. | Hybrid aircraft wheel having metal and composite portions |
CN111923452A (en) * | 2020-06-22 | 2020-11-13 | 成都飞机工业(集团)有限责任公司 | Forming method for controlling curing deformation of composite material hyperboloid skin |
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